Titan 340CC Operation Manual page 8

Weight
Coils + Bracket + Hardware
Starter Ring Gear and Support
1
Basic Engine Configuration:
• Cub Crafters oil sump and induction tubes
• Hollow front main crankshaft with plug for fixed pitch propeller
* Starter ring gear and support, caburetor, magnetos, ignition system and spark plugs not included.
The plasma II is not included because it is installed on the airframe.
2
Arm Datum is the front of the propeller ring gear support.
Method for Computing Engine Weight and Center of Gravity:
1 Start with basic engine weight and moment.
2 Add or subtract weight and moment of components added or removed.
3
The new total moment is divided by the new total weight to establish the new
complete engine center of gravity.
8 | Copyright © 2015 Airmotive Engineering Corp.
Component
Basic Engine
1
Add Oil Filter
Add the Starter
Add the Alternator
MA4-SPA Carburetor
Ignition Harness
Spark Plugs
Total Weight and Moment
Weight Arm
2
223.00 14.50
1.39 29.30
7.85 4.97
5.50 4.97
3.50 18.80
1.50 14.30
1.32 13.98
1.75 12.48
5.50 1.90
251.3
Moment
3,233.50
40.73
39.01
27.34
65.80
21.45
18.45
21.84
10.45
3,478.57